Problems encountered in developing a high speed trajectory data processor for the shuttle ascent and entry phases are described. The development of a 19 state acceleration filter for the processor is reported.
Space shuttle navigation filter development
1976-08-03
Report
No indication
English
Space Shuttle Navigation Filter Development
NTIS | 1976
|Space Shuttle navigation validation
AIAA | 1985
|Space shuttle navigation analysis
NTRS | 1976
|Space Shuttle Navigation Analysis
NTIS | 1976
|